Components and Characteristics of the Instrument Landing System (ILS)
T-45A UJPT & E2-C2 INav-04
(2) indicates a position approximately 3,500 ft from the landing
threshold and approximately 200 ft AGL above the touch-
down zone
(3) Identification is a coded audio tone (continuous alternating
dots and dashes) and flashing amber cockpit marker light
c.
Inner Marker (IM)
(1) Indicates a point that an aircraft flying a Category II or III
ILS approach is at the designated decision height (DH) on
glidepath between the MM and the landing threshold
(2) Aircraft is approximately 100 ft AGL at IM if on glidepath
and FAC
(3) Identified by a coded audio tone (continuous dots) and a
flashing white cockpit marker beacon light
d.
Back Course (BC)
(1) A BC marker beacon normally indicates an LOC BC final
approach fix (FAF) where the approach glideslope is
intercepted and the descent is commenced
(2) Identified by a coded audio tone (two dots continuously
repeating) and a flashing white cockpit marker light
5.
Marker beacon tones
Fig 3: Marker Beacon
Code/Color
a.
Marker beacons emit specific coded tones, at different pitches,
Identification Table
which the pilot of an ILS/LOC equipped aircraft can monitor
when on the final approach course
b.
In the T-45A, marker beacon tones may be monitored by
to the "ON" position
c.
MKR audio tone volume in the T-45A is preset and cannot be
controlled by the RCVR volume control knob on the
B. Distance Measuring Equipment (DME)
1.
When DME is automatically coupled to the ILS frequency and
specified in the approach procedure, DME may be used:
a.
In lieu of the OM
b.
As a BC final approach fix (FAF)
c.
To establish other fixes on the localizer course
(6-99) Original
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